Composite Helicopter

Manufacturer:

Composite Helicopter

Country:

New Zealand

Commercial designation:

Adventourer

Technical designation:

KC518

Version, Variant:

C20

Type:

Fenestron

Currently produced:

Y

Typical missions:

Proto

Flight conditions:

VFR

First flight:

0

Landing system:

skids

Blades number:

4

Tail blades number:

4

MTOW with external loads:

1450 kg

3197.25 lbs

MTOW with only internal loading:

1450 kg

3197.25 lbs

Empty weight:

790 kg

1741.95 lbs

External payload:

567 kg

1250.235 lbs

Internal payload:

652 kg

1437.66 lbs

Standard fuel tank:

300 kg

661.5 lbs

with optionnal external fuel tank:

424 kg

934.92 lbs

Cruise speed:

250 km/h

135 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

296 km/h

159.84 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

0 km

0 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

03:36:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

5 m/s

984 ft/min

IGE max hovering altitude, MTOW:

3000 m

9840 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

2300 m

7544 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

0 m

0 ft

Max operating altitude, empty weight:

4600 m

15088 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Rolls-Royce

Model:

250-C20B

Engines quantity:

1

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

0 kW

0 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

0 m

0 ft

Rotor diameter:

9 m

29.52 ft

Tail rotor diameter:

0.97 m

3.1816 ft

Fuselage length:

8.8 m

28.864 ft

Overall height:

3.5 m

11.48 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

1

Max pax number:

5

Average price:

0 $